The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 28, 2022

Filed:

Aug. 26, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:
Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/047 (2006.01); F01D 5/28 (2006.01); F01D 5/14 (2006.01); F04D 29/38 (2006.01); B32B 5/02 (2006.01); B32B 5/26 (2006.01); B32B 38/18 (2006.01); B32B 3/06 (2006.01); B32B 5/12 (2006.01); B32B 7/02 (2019.01); B32B 19/02 (2006.01); B32B 19/06 (2006.01); B32B 3/08 (2006.01); B29C 70/88 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); B32B 5/02 (2013.01); B32B 5/26 (2013.01); B32B 38/1808 (2013.01); F01D 5/14 (2013.01); F01D 5/282 (2013.01); F01D 5/288 (2013.01); B32B 2307/20 (2013.01); B32B 2603/00 (2013.01); F05D 2220/32 (2013.01); F05D 2230/00 (2013.01); F05D 2260/407 (2013.01); F05D 2300/224 (2013.01); F05D 2300/603 (2013.01);
Abstract

Composite components and methods for forming composite components are provided. For example, a composite component of a gas turbine engine comprises a composite material, a plurality of piezoelectric fibers, and an anti-icing mechanism. The anti-icing mechanism is in operative communication with the piezoelectric fibers such that the anti-icing mechanism is activated by one or more electrical signals from the piezoelectric fibers. In exemplary embodiments, the composite component is a composite airfoil and the anti-icing mechanism is one or more heating elements. Methods for forming composite components may comprise forming piezoelectric plies comprising piezoelectric fibers embedded in a matrix material; forming reinforcing plies comprising reinforcing fibers embedded in the matrix material; laying up the piezoelectric and reinforcing plies to form a ply layup; and processing the ply layup to form the composite component. Methods including forming a piece of piezoelectric material that is adhered to a composite component also are provided.


Find Patent Forward Citations

Loading…